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Millimeter Wave RADAR Power-Range Spectra Interpretation    51

                              2.4.2.1 Thermal noise
                              Thermal noise is generated in the RADAR receiver electronics. The noise power
                              is given by P N (in Watts), where

                                                        P N = kT 0 β                    (2.8)

                              where k is the Boltzmann constant, T 0 is the temperature, and β is the receiver
                              bandwidth [22]. As shown in Section 2.3, the power in the beat frequency
                              signal (found from the FFT of this signal) is affected by the thermal noise power

                              a R (t−τ), which contributesto A in Equation(2.6). Itcan beshown by analyzing
                              the transition of this thermal (Gaussian) noise through the entire FMCW range
                              detection process that when a target is present (strong received signal) the noise
                              in the power–range spectrum follows a Gaussian distribution. When no target
                              is present (weak or no reflected signal) it will be demonstrated from the results
                              that the noise power follows a Weibull distribution. Therefore measurements
                              with target presence/absence were made to verify these distributions and to
                              quantify the power variance during target absence/presence.


                              2.4.2.2 Phase noise
                              Another source of noise which affects the range spectra is the phase noise. The
                              phase noise is generated by the frequency instability of the oscillator due to
                              the thermal noise. Ideally for a particular input voltage to the VCO, the output
                              has a single spectral component. In reality, the VCO generates a spectrum
                              of frequencies with finite bandwidth which constitutes phase noise. This is
                              shown in Equation (2.6), where a band of noise frequencies with different phase
                              components,  φ(t, τ) affects the desired signal frequency, which corresponds
                              to range. The phase noise broadens the received power peaks and reduces the
                              sensitivity of range detection [11] as shown in Figure 2.4. 3  This introduces
                              noise into the range estimate itself. Experimental data provides insight into the
                              phase noise distribution. For predicting the RADAR range spectra, the peaks at
                              predicted targets are broadened by a small constant amount. This broadening
                                                                               4
                              is based on real measurements, which have shown the peaks to have widths
                              ranging from 2.5 to 3.5 m. This has been observed from targets, of different
                              RCS, placed at different distances from the RADAR.
                                 Figure 2.5 shows 1000 superimposed range bins obtained for the same
                              RADAR swash plate bearing angle. Figure 2.5a shows the entire range bins
                              over the full 200 m range,  while Figure 2.5b shows a zoomed view of the
                              spectra obtained from the feature at 10.25 m. From the figures, it is evident that
                              3  The peaks and skirts shown in Figure 2.4 occur due to the leakage of signals from the transmitter
                              into the mixer through the circulator and also due to the antenna impedance mismatch [11].
                              4  At their intersections with the high pass filter gain curve shown in Figure 2.3.




                              © 2006 by Taylor & Francis Group, LLC



                                 FRANKL: “dk6033_c002” — 2006/3/31 — 17:29 — page 51 — #11
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